View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48481U 26145.43396088 +.00000000 +00000-0 +52641-4 0 00009
2 48481 53.1576 196.5501 0001393 80.7316 279.3843 15.31705589 02
| Epoch (UTC): | 25 May 2026 10:24:54 |
| Eccentricity: | 0.0001393 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 196.5501° |
| argument of perigee: | 80.7316° |
| revolutions per day: | 15.31705589 |
| mean anomaly at epoch: | 279.3843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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